Blackburn T.5 Ripon

The Ripon was a torpedo-bomber with a steel-tube fuselage and wooden wings, first flown as the Ripon I in 1926. The first of 20 aerodynamically cleaner Ripon IIs replaced the Blackburn Darts of Nos 460, 461 and 462 Flights, FAA, on board HMS Glorious and Furious in 1929.

Forty Ripon IIAs with shorter-span duralumin wing-ribs and smaller rudders were built during 1930-31. Five of these belonging to No 460 Flight went to Buenos Aires on board HMS Eagle in 1931 and were used for formation flying over the British Empire Exhibition during March and April. Thirty-one Ripon IICs with additional sweep-back and steel wing-spars were delivered during 1931-32. Earlier marks were thereafter returned to Blackburn for modification to this standard. Ripon IICs formed the equipment of Nos 465 and 466 Flights on board Furious in 1931, but in 1933 all the Flights were regrouped. The IICs remained in service until 1934.

One Ripon IIF, with a Bristol Jupiter radial engine, was delivered to Finland in September 1929, where 25 others were constructed with plywood-covered fuselages and wheel/float/ski landing gears. These saw service against the Russians during the 1939 ‘Winter War’.

Gallery

Ripon IIA
Engine: 1 x Napier Lion XIA, 425kW
Take-Off Weight: 3359 kg / 7405 lb
Wingspan: 13.67 m / 44 ft 10 in
Length: 11.2 m / 36 ft 9 in
Height: 3.91 m / 12 ft 10 in
Wing Area: 63.45 sq.m / 682.97 sq ft
Max. Speed: 203 km/h / 126 mph
Cruise Speed: 175 km/h / 109 mph
Ceiling: 3000 m / 9850 ft
Range W/Max.Fuel: 1705 km / 1059 miles
Armament: 2 x 7.7mm machine-guns, one torpedo or 680kg of bombs

Blackburn RB.1 Iris

Iris III

The Blackbrn Iris was designed as a long range, ocean going aircraft to augment the coastal patrol services Supermarine Southamptons. Only one squadron was equipped with Iris aircraft, first with the Mk.III which later, by modification, became the Mk.V, and ultimately with what might have been a later mark, but was designated “Perth”.
The Armament of the Iris consisted of Lewis guns in bow and midship positions with a third one at the tail end of the hull which had only a limited arc of fire. In the bow position, a one pounder gun, made by the Coventry Ordnance Works and consequently known as the Cow gun, could be mounted, and was once every year for demonstration purposes.
The five-seat Iris was a biplane flying-boat. The first of only eight built flew on 19 June 1926. The single Iris I, powered by three 484.4kW Rolls-Royce Condor III engines, was converted into the II with 503kW Condor IIIA. It was followed by four Iris III with 503kW Condor IIIB engines (entering service with the RAF in 1930); a single Mk IV (the first prototype with 596kW Armstrong Siddeley Leopard Ill, mounted as two tractors and one pusher); and three V with 615kW (825 hp) Rolls-Royce Buzzard IIMS engines. A III was also brought up to V standard and the luxury of a roof over the pilot’s positions. No heating.

Iris I
Engines: three 484.4kW Rolls-Royce Condor III

Iris II
Engines: 3 x 503kW Condor IIIA

R.B.1B “Iris” III
Engine: 3 x Rolls-Royce “Condor” IIIB, 503kW, 675 hp
Take-Off Weight: 13376 kg / 29489 lb
Empty Weight: 8640 kg / 19048 lb
Wingspan: 29.57 m / 97 ft 0 in
Length: 20.54 m / 67 ft 5 in
Height: 7.77 m / 25 ft 6 in
Wing Area: 207.07 sq.m / 2228.88 sq ft
Max. Speed: 190 km/h / 118 mph
Cruise Speed: 156 km/h / 97 mph
Ceiling: 3230 m / 10600 ft
Range W/Max.Fuel: 1287 km / 800 miles
Crew: 5
Armament: 3 x 7.7mm machine-guns, 900kg bombs

Iris V
Engines: 3 x Rolls-Royce Buzzard, 825 hp.

Blackburn T.3 Velos

In 1925 the Blackburn Aeroplane & Motor Co concluded an arrangement with the Greek Government to organise an aircraft factory at Phaleron, near Athens, Greece. The EAF / State Aircraft Factory constructed a series of Velos two seat torpedo planes, designed by Blackburn; a series of Armstrong Whitworth Atlas two seat fighters; and a series of Avro 504O and 504N trainers.

Greek built Velos taking off in Phaleron Bay

Engine: 1 x 450hp Napier Lion V
Take-Off Weight: 2815 kg / 6206 lb
Empty Weight: 1766 kg / 3893 lb
Wingspan: 14.78 m / 48 ft 6 in
Length: 10.82 m / 35 ft 6 in
Height: 3.73 m / 12 ft 3 in
Wing Area: 60.76 sq.m / 654.01 sq ft
Max. Speed: 172 km/h / 107 mph
Ceiling: 4298 m / 14100 ft
Range: 580 km / 360 miles
Crew: 2
Armament: 1 x 7.7mm machine-gun, 4 x 100kg bombs or a torpedo

Blackburn L.1 Bluebird

Bluebird IV

The Blackburn Bluebird was the first British side-by-side two-seater to enter production and 79 were built in various marks with engines ranging from 80 to 100hp.

The Bluebird was of metal frame construction and used a 100 hp de Havilland Gipsy I engine. The streamlined fuselage was fabric covered, and the two seats were side-by-side. Dual controls were fitted.

Not only was the Bluebird manufactured by Blackburn, but also by Saunders-Roe at Cowes. Wings were also sub-contracted by Suanders-Roe to Boulton & Paul Ltd of Norwich. The Saunders-Roe aircraft sales were handled by Auto-Auctions Ltd.

The L.1C Bluebird IV sold for £795, later reduced to £695.

The Hon Mrs Victor Bruce flew one solo around the world between 25 September 1930 and 20 February 1931.

Bluebird IV:
Engine: Armstrong Siddeley Genet Major

L.1C Bluebird IV
Engine: 100 hp de Havilland Gipsy I
Max level speed: 120 mph
Cruise speed: 85 mph
Max ceiling: 15,000 ft
Max range: 320 miles
Seats: 2 side-by-side

Blackburn Pellet

Robert Blackburn announced in March 1923 that his company, the Blackburn Aeroplane and Motor Co Ltd of Leeds, was to build an entry for the 1923 Schneider Trophy Contest, and the event was set for 28 September, with Cowes, on the Isle of Wight, as the starting and finishing point. The aircraft was to be a single-seat flying boat and the company had only worked on one flying boat – before, the NAB single-seat fleet escort bomber of 1918 and that had never been completed.
Blackburn’s chief test pilot, Reginald W. Kenthworthy, wanted the aircraft to be ready for test flying in August, a month before the race, so that any problems could be resolved and he could gain some handling experience on an untried prototype.

The design of the aircraft was largely determined by the use of the hull of the NAB, a streamlined structure which comprised circular wooden formers separated by stringers and planked with diagonal mahogany strips in two layers crossing each other at right angles. The Pellet’s hull, adapted from the abandoned N.1B fleet escort bomber, featured Linton Hope’s smooth, two-step mahogany construction. The aircraft had a compact biplane layout with a Napier Lion engine perched above the top wing. Flush radiators cooled it, and the pilot sat ahead of the propeller. To this hull was added, a biplane wing structure, comprising single-bay sesquiplane wings, the lower wing being of less span and chord than the upper and having no ailerons. The wing structure was attached to the top of the hull and on the top centre section, supported by N struts, was
mounted a 450 hp Napier Lion, in a close fitting, streamlined nacelle. It was the engine from the Gloster Bantel, which had won that year’s Aerial Derby. Wooden wingtip floats were fitted beneath the outboard N struts of the narrow-gap wings. The open cockpit had a well raked windscreen and there was a streamlined fairing behind the he pilot’s head. A strut-braced tailplane was Positioned half-way up to the fin.
The flying boat was eventually named the Pellet and the civil registration G-EBHF was allotted to it on 23 July.
Despite efforts to complete the Pellet on time, its engine was not available until August and it was not finished until the first week of September. After some engine runs it was launched down the Brough shipway with Kenworthy in the cockpit. Unfortunately, it was caught by the Humber tide and the crosswind, dipped its starboard wingtip float and turned turtle and sank, ejecting Kenworthy into the river.
It was only three weeks before the contest, but Robert Blackburn was undeterred. The Pellet was stripped, repaired and given larger wingtip floats and the engine was returned to Napiers for cleaning. Five days before the event, the Pellet was again ready, but, as there was no time to fly it at Brough, it was sent by rail to Fairey’s yard at Hamble, Southampton, for assembly and testing.
On 26 September, only two days before the contest and the day before the preliminary tests, the Pellet was relaunched, now displaying the racing number 6 on its fuselage and rudder. During the take-off run it shipped a lot of water, but took off successfully. Kenworthy then found that he needed all of his strength on the control column to prevent the Pellet diving, as it was extremely nose-heavy. To complicate matters, the wing-mounted recessed radiators proved inadequate and the cooling water boiled. With no choice but to alight, Kenworthy put the troublesome machine down on the sea just past the RAF seaplane base at Calshot and was eventually retrieved by a motor boat from S.E. Saunders Lid, which towed it to Cowes.
Working through the night, Saunders’ staff fitted a large Lamblin ‘crab-pot’ radiator beneath the engine nacelle and bypassed the wing radiators. The original two-bladed wooden aircrew had been damaged by spray so a two-bladed metal unit was, installed. The fin chines were reinforced and adjustments were also made in an attempt to settle the problem with the centre of gravity.
By 11.48 next morning, just before the final launching time for the navigability and watertightness tests, the Pellet was ready, However, as Kenworthy began his takeoff run down the River Medina, a heavy swell turned the machine slightly to the right so that it was heading straight for two rowing boats. Kenworthy tried to change direction: ‘the machine, travelling at about 140 mph jumped and jumped’, Kenworthy told a Daily Graphic reporter. It then left the water in a stalled attitude, coming down twice with great force before it tipped over to starboard. The wingtip float touched the water and the Pellet made a final leap before diving nose down and turning right over.

Kenworthy was picked up unharmed by Lord Montagu of Beaulieu in his motor boat, fainted and was revived by artificial respiration. He had been under the hull for 61 seconds. The Saunders works manager, Mr Newman, recovered the Pellet that night, but this time it was beyond repair. Robert Blackburn never built another Schneider Trophy racer.

Engine: One 450 hp Napier Lion W-12
Upper span: 34 ft
Lower span: 29 ft 6 in
Length: 28 ft 7 in
Height: 10 ft 8 in
Maximum speed (estimated): 122 mph

Blackburn R.1 Blackburn

The Blackburn was a 1922 carrier-borne Fleet spotter-reconnaissance biplane, accommodating a pilot in an open cockpit in front of the upper wing leading edge. A wireless operator/gunner and a navigator/observer were provided with a cabin inside the fuselage and only needed to venture out into the open for observation or to use the rear-mounted Lewis machine-gun. Thirty production Blackburn Is, with 335kW Napier Lion IIB engines, were built. The type first entered service on board HMS Eagle in 1923. These were followed by 29 346kW Napier Lion-engined Blackburn IIs, entering service in 1926. All were replaced by Fairey IIIFs in 1931.

Blackburn II
Engine: 346kW Napier Lion
Take-off weight: 3,022 kg / 6648 lb
Wingspan: 13.87 m / 45 ft 6 in
Length: 11.02 m / 36 ft 2 in
Max. speed: 157 km/h / 98 mph
Armament: 2 x 7.7mm machine-guns

Blackburn T.2 Dart

The 1921 Dart was the FAA’s standard single-seat torpedo bomber from 1923 to 1933. Similar to the Blackburn Swift but with reduced wing span, it could carry a torpedo or underwing bombs.

A batch of 32 were ordered by the Fleet Air Arm in August 1924.

The Dart first entered service with No 460 Flight in 1923 on board HMS Eagle, stationed in the Mediterranean; and with Nos 461 and 462 on board HMS Furious, based in home waters. Shore training was by D3 Flight at Gosport. The aircraft’s low stalling speed of 70km/h enabled it to pioneer the technique of deck landing by night on HMS Furious in 1926. In 1928 Nos 463 and 464 Flights embarked on HMS Courageous for service in the Mediterranean and in the following year a single example was delivered to No 36 Squadron, RAF, for smoke-screen trials. Three Darts were also converted into two-seat advanced-training seaplanes for use on the River Humber by Blackburn’s RAF Reserve School, being used between 1925 and 1929.

Production ended in 1928 after the 117th Dart had been completed.

Engine: 1 x Napier Lion IIB, 335kW
Take-Off Weight: 2898 kg / 6389 lb
Empty Weight: 1634 kg / 3602 lb
Wingspan: 13.87 m / 45 ft 6 in
Length: 10.77 m / 35 ft 4 in
Height: 3.94 m / 12 ft 11 in
Wing Area: 60.76 sq.m / 654.01 sq ft
Max. Speed: 172 km/h / 107 mph
Ceiling: 3109 m / 10200 ft
Range: 483 km / 300 miles
Armament: 1 x 240kg bomb or a torpedo